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    HITCAN for Actively Cooled Hot-Composite Thermostructural Analysis

    Source: Journal of Engineering for Gas Turbines and Power:;1992:;volume( 114 ):;issue: 002::page 315
    Author:
    C. C. Chamis
    ,
    S. N. Singhal
    ,
    J. J. Lackney
    ,
    P. L. N. Murthy
    DOI: 10.1115/1.2906589
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A computer code, HITCAN (High Temperature Composite Analyzer) has been developed to analyze/design hot metal matrix composite structures. HITCAN is a general purpose code for predicting the global structural and local stress-strain response of multilayered (arbitrarily oriented) metal matrix structures both at the constituent (fiber, matrix, and interphase) and the structure level and including the fabrication process effects. The thermomechanical properties of the constituents are considered to be nonlinearly dependent on several parameters, including temperature, stress, and stress rate. The computational procedure employs an incremental iterative nonlinear approach utilizing a multifactor-interaction material behavior model, i.e., the material properties are expressed in terms of a product of several factors that affect the properties. HITCAN structural analysis capabilities (static, load stepping—a multistep static analysis with material properties updated at each step, modal, and buckling) for cooled hot structures are demonstrated through a specific example problem.
    keyword(s): Composite materials , Stress , Materials properties , Design , Computers , Buckling , High temperature , Fibers , Manufacturing , Metal matrix composites , Temperature , Metals AND Structural analysis ,
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      HITCAN for Actively Cooled Hot-Composite Thermostructural Analysis

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/110242
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorC. C. Chamis
    contributor authorS. N. Singhal
    contributor authorJ. J. Lackney
    contributor authorP. L. N. Murthy
    date accessioned2017-05-08T23:38:27Z
    date available2017-05-08T23:38:27Z
    date copyrightApril, 1992
    date issued1992
    identifier issn1528-8919
    identifier otherJETPEZ-26699#315_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/110242
    description abstractA computer code, HITCAN (High Temperature Composite Analyzer) has been developed to analyze/design hot metal matrix composite structures. HITCAN is a general purpose code for predicting the global structural and local stress-strain response of multilayered (arbitrarily oriented) metal matrix structures both at the constituent (fiber, matrix, and interphase) and the structure level and including the fabrication process effects. The thermomechanical properties of the constituents are considered to be nonlinearly dependent on several parameters, including temperature, stress, and stress rate. The computational procedure employs an incremental iterative nonlinear approach utilizing a multifactor-interaction material behavior model, i.e., the material properties are expressed in terms of a product of several factors that affect the properties. HITCAN structural analysis capabilities (static, load stepping—a multistep static analysis with material properties updated at each step, modal, and buckling) for cooled hot structures are demonstrated through a specific example problem.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleHITCAN for Actively Cooled Hot-Composite Thermostructural Analysis
    typeJournal Paper
    journal volume114
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2906589
    journal fristpage315
    journal lastpage320
    identifier eissn0742-4795
    keywordsComposite materials
    keywordsStress
    keywordsMaterials properties
    keywordsDesign
    keywordsComputers
    keywordsBuckling
    keywordsHigh temperature
    keywordsFibers
    keywordsManufacturing
    keywordsMetal matrix composites
    keywordsTemperature
    keywordsMetals AND Structural analysis
    treeJournal of Engineering for Gas Turbines and Power:;1992:;volume( 114 ):;issue: 002
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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